Performance Database
 |
|
GULFSTREAM G-IV |
|
Engines |
|
| Make | Rolls Royce |
| Model | TAY MK 611-8/TAY MK 610-8 |
| HP/Thrust lbs per engine | 13.850 |
| TBO (hours) | 8.000 |
Fuselage Dimension |
|
| Length (ft) | 88.30 |
| Height (ft) | 24.40 |
| Wing Span (ft) | 77.80 |
| Passengers | 14 + 2 Crew |
| Pressurization (psi) | 9.5 |
Weights (lbs) |
|
| Max Ramp | 73.600 |
| Max Takeoff | 73.200 |
| Zero Fuel | 46.500 |
| Basic Operating | 42.650 |
| Max Landing | 58.500 |
Fuel Capacity |
|
| Standard lbs/gal | 29.500 / 4.403 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 5.280 |
| 5000 +20C BFL (ft) | 7.985 |
Landing Performance (ft) |
|
| FAA Field Length | 3.377 |
Range (NM) |
|
| Max Range | 4.220 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 4.219 |
| Engine Out (fpm) | 1.198 |
Speeds (Knots) |
|
| Vmc | 125 |
| Vso (Landing) | 116 |
| Normal Cruise TAS | 460 |
| Vmo (Max Operating) IAS | 340 |
Ceiling (ft) |
|
| Certified Ceiling | 45.000 |
Specifications are provided as introductory information only and
are subject to verification by the buyer during a prepurchase inspection
of the aircraft. The aircraft is offered subject to prior sale,
price changes and/or removal from the market without notice.
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